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SA7024 (sa7024-il)

SA7024 - Selig / Ashok Gopalarathnam SA7024 low Reynolds number airfoil


Airfoil sa7024-il
Details Dat file Parser  
(sa7024-il) SA7024
Selig / Ashok Gopalarathnam SA7024 low Reynolds number airfoil
Max thickness 7% at 25.9% chord.
Max camber 3.3% at 43.3% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Selig format
SA7024
       1.00000      .00000
        .99820      .00029
        .99296      .00127
        .98456      .00298
        .97328      .00531
        .95928      .00803
        .94257      .01096
        .92315      .01411
        .90116      .01753
        .87679      .02117
        .85023      .02497
        .82165      .02889
        .79126      .03288
        .75924      .03686
        .72579      .04078
        .69115      .04460
        .65551      .04824
        .61909      .05166
        .58210      .05481
        .54479      .05763
        .50733      .06007
        .46996      .06212
        .43289      .06369
        .39632      .06477
        .36045      .06535
        .32549      .06539
        .29159      .06485
        .25893      .06376
        .22772      .06210
        .19806      .05986
        .17009      .05707
        .14398      .05377
        .11982      .04993
        .09767      .04563
        .07768      .04094
        .05989      .03587
        .04433      .03049
        .03104      .02498
        .02012      .01940
        .01158      .01386
        .00540      .00851
        .00158      .00354
0.0 0.0
        .00166     -.00362
        .00686     -.00589
        .01518     -.00796
        .02645     -.00964
        .04065     -.01082
        .05781     -.01156
        .07781     -.01189
        .10057     -.01180
        .12597     -.01135
        .15388     -.01057
        .18414     -.00950
        .21657     -.00818
        .25098     -.00667
        .28717     -.00501
        .32492     -.00326
        .36398     -.00147
        .40410      .00029
        .44502      .00196
        .48645      .00350
        .52813      .00484
        .56970      .00589
        .61079      .00666
        .65110      .00720
        .69038      .00752
        .72834      .00763
        .76472      .00754
        .79926      .00727
        .83172      .00682
        .86187      .00624
        .88949      .00555
        .91441      .00479
        .93644      .00397
        .95544      .00313
        .97125      .00228
        .98372      .00146
        .99273      .00074
        .99818      .00021
       1.00000     0.00000
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Polars for SA7024 (sa7024-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   sa7024-il50,000938.8 at α=6°Mach=0 Ncrit=9Xfoil predictionDetails
   sa7024-il50,000542.3 at α=5.5°Mach=0 Ncrit=5Xfoil predictionDetails
   sa7024-il100,000959.8 at α=4.75°Mach=0 Ncrit=9Xfoil predictionDetails
   sa7024-il100,000559 at α=4.5°Mach=0 Ncrit=5Xfoil predictionDetails
   sa7024-il200,000980.5 at α=4°Mach=0 Ncrit=9Xfoil predictionDetails
   sa7024-il200,000574.6 at α=4°Mach=0 Ncrit=5Xfoil predictionDetails
   sa7024-il500,0009105.7 at α=3.75°Mach=0 Ncrit=9Xfoil predictionDetails
   sa7024-il500,000593.9 at α=3.75°Mach=0 Ncrit=5Xfoil predictionDetails
   sa7024-il1,000,0009122.4 at α=3.25°Mach=0 Ncrit=9Xfoil predictionDetails
   sa7024-il1,000,0005107.2 at α=3.25°Mach=0 Ncrit=5Xfoil predictionDetails
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